Spacecraft entry monitoring system /EMS/ gives a rectilinear display of acceleration load factor and velocity information. This allows an astronaut to respond with manual spacecraft attitude corrective maneuver commands.


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    Title :

    Rectilinear display gives acceleration load factor and velocity information


    Contributors:

    Publication date :

    1967-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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